A satellite is any object that is orbiting the earth, sun or
other massive body. Satellites can be categorized as natural
satellites or man-made satellites. The moon, the planets and
comets are examples of natural satellites. Accompanying the orbit of natural
satellites are a host of satellites launched from earth for purposes of
communication, scientific research, weather forecasting, intelligence, etc. Whether
a moon, a planet, or some man-made satellite, every satellite's motion is
governed by the same physics principles and described by the same mathematical
equations.
The fundamental principle to be understood concerning
satellites is that a satellite is a projectile. That is to say,
a satellite is an object upon which the only force is gravity. Once launched
into orbit, the only force governing the motion of a satellite is the force of gravity.
Newton was the first to theorize that a projectile launched with sufficient
speed would actually orbit the earth. Consider a projectile launched
horizontally from the top of the legendary Newton’s Mountain - at a
location high above the influence of air drag. As the projectile moves
horizontally in a direction tangent to the earth, the force of gravity would
pull it downward. And as mentioned in Lesson 3, if the launch
speed was too small, it would eventually fall to earth. The diagram at the
right resembles that found in Newton's original writings. Paths A and B
illustrate the path of a projectile with insufficient launch speed for orbital
motion. But if launched with sufficient speed, the projectile would fall
towards the earth at the same rate that the earth curves. This would cause the
projectile to stay the same height above the earth and to orbit in a circular
path (such as path C). And at even greater launch speeds, a
cannonball would once more orbit the earth, but now in an elliptical path (as
in path D). At every point along its trajectory, a
satellite is falling toward the earth. Yet because the earth curves, it never
reaches the earth.
So what launch speed does a satellite need in order to orbit
the earth? The answer emerges from a basic fact about the curvature of the
earth. For every 8000 meters measured along the horizon of the earth, the
earth's surface curves downward by approximately 5 meters. So if you were to
look out horizontally along the horizon of the Earth for 8000 meters, you would
observe that the Earth curves downwards below this straight-line path a
distance of 5 meters. For a projectile to orbit the earth, it must travel
horizontally a distance of 8000 meters for every 5 meters of vertical fall. It so happens that the vertical distance that
a horizontally launched projectile would fall in its first second is
approximately 5 meters (0.5*g*t2). For this reason, a projectile
launched horizontally with a speed of about 8000 m/s will be capable of
orbiting the earth in a circular path. This assumes that it is launched above
the surface of the earth and encounters negligible atmospheric drag. As the
projectile travels tangentially a distance of 8000 meters in 1 second, it will
drop approximately 5 meters towards the earth. Yet, the projectile will remain
the same distance above the earth due to the fact that the earth curves at the
same rate that the projectile falls. If shot with a speed greater than 8000
m/s, it would orbit the earth in an elliptical path.
The motion of an orbiting satellite can be described by the
same motion characteristics as any object in circular motion. The velocity of the
satellite would be directed tangent to the circle at every point along its
path. The acceleration of the satellite would be directed towards
the center of the circle - towards the
central body that it is orbiting. And this acceleration is caused by a net force that is
directed inwards in the same direction as the acceleration.
This centripetal force is supplied by gravity -
the force that universally acts at a distance between any two objects that
have mass. Were it not for this force, the satellite in motion would continue
in motion at the same speed and in the same direction. It would follow its
inertial, straight-line path. Like any projectile, gravity alone influences the
satellite's trajectory such that it always falls below its straight-line,
inertial path. This is depicted in the diagram below.
Observe that the inward net force pushes (or pulls) the satellite (denoted by
blue circle) inwards relative to its straight-line path tangent to the circle.
As a result, after the first interval of time, the satellite is positioned at
position 1 rather than position 1'. In the next interval of time, the same
satellite would travel tangent to the circle in the absence of gravity and be
at position 2'; but because of the inward force the satellite has moved to
position 2 instead. In the next interval of time, the same satellite has moved
inward to position 3 instead of tangentially to position 3'. This same
reasoning can be repeated to explain how the inward force causes the satellite
to fall towards the earth without actually falling into it.
Occasionally satellites will orbit in paths that can be
described as ellipses. In such cases, the central body is located at
one of the foci of the ellipse. Similar motion characteristics apply for
satellites moving in elliptical paths. The velocity of the satellite is
directed tangent to the ellipse. The acceleration of the satellite is directed
towards the focus of the ellipse. And in accord with Newton's
second law of motion, the net force acting upon the satellite is
directed in the same direction as the acceleration - towards the focus of the
ellipse. Once more, this net force is supplied by the force of gravitational
attraction between the central body and the orbiting satellite. In the case of
elliptical paths, there is a component of force in the same direction as (or
opposite direction as) the motion of the object. such a
component of force can cause the satellite to either speed up or slow down in addition to changing directions. So
unlike uniform circular motion, the elliptical motion of satellites is not
characterized by a constant speed.
In summary, satellites are projectiles that orbit around a
central massive body instead of falling into it. Being projectiles, they are
acted upon by the force of gravity - a universal force that acts over even
large distances between any two masses. The motion of satellites, like any
projectile, is governed by Newton's laws of motion. For this reason, the
mathematics of these satellites emerges from an application of Newton's
universal law of gravitation to the mathematics of circular motion. The mathematical
equations governing the motion of satellites.
1. The fact that satellites can maintain their motion and
their distance above the Earth is fascinating to many. How can it be? What
keeps a satellite up?
One might think
that an inward force would move a satellite right into the center of the circle; but that's only the case if the
satellite were in a rest position. Being that the satellite is already in
motion in a tangential direction, the inward force merely turn from its
straight-line tangential direction. Instead of turning and falling into the
earth, it turns and curves around the earth (thanks to the fact that the earth
is round.)
2. If there is an inward force acting upon an earth orbiting
satellite, then why doesn't the satellite collide into the Earth?
The previous
question provides most of the reasoning for this. A combination of a tangential
velocity and a curved earth prevents this collision. If it is your belief that
the direction an object moves is always in the same direction of the force,
then you have a misconception. Lots of objects move in a direction different
from a force. For instance as your car heads east and and slam
on your brakes, the force on the car is westward; only the acceleration would
be westward. And for satellites, the direction of motion is tangential and the
force is inward; only the acceleration is inward and this cause the circular
motion around the central body.